Oscillatory Combustion in Rockets Semiannual Report, 1 Jun. - 30 Nov. 1968
The Flow of a Rarefied, Dissociated Gas over a Sharp Flat Plate
Analytical study of He II flow characteristics in the SHOOT transfer line
Analysis of a redundant free-flying spacecraft/manipulator system
Efficient Calculation of Radiation Heat Transfer in Participating Media
Boundary Conditions for Acoustic Eigenmodes Computation in Gas turbine Combustion Chambers
Stability Analysis of Solid Rocket Motor Combustion by Computational Fluid Dynamics
Calculation of Multidimensional Flames Using Large Chemical Kinetics
Effects of Scalar Dissipation Rate Fluctuations on Autoignition of Hydrogen/Air Mixture
Comparison of Direct and Indirect Combustion Noise Mechanisms in a Model Combustor
Development and Verification of a One-Dimensional Ablation Code Including Pyrolysis Gas Flow
Additional Description of Laminar Heat Convection in Tube with Uniform Wall Temperature
Acoustic Scattering by a Localized Thermal Disturbance
Modeled Lattice Boltzmann Equation and the Constant-Density Assumption